This paper provides an efficient and accurate numerical method for computing internal flows in two dimensions. The method has been designed to deal with subsonic-to-supersonic flows without shocks, but can deal with entirely subsonic and transonic flows. The perturbative lambda formulation equations are considered and solved by block-line-relaxation methods. The validity of the proposed technique is demonstrated for a well documented nozzle flow problem for both subsonic and subsonic-to-supersonic flow conditions.
|Titolo:||Efficient Solution of Compressible Internal Flows|
|Titolo del libro:||Modern Research Topics in Aerospace Propulsion : in Honor of Corrado Casci|
|Data di pubblicazione:||1991|
|Digital Object Identifier (DOI):||http://dx.doi.org/10.1007/978-1-4612-0945-4_11|
|Appare nelle tipologie:||2.1 Contributo in volume (Capitolo o Saggio)|